The Open Aerospace Engineering Journal
2013, 6 : 6-19Published online 2013 October 11. DOI: 10.2174/1874146001306010006
Publisher ID: TOAEJ-6-6
Selecting Design Objectives for an Integrated Guidance System of a Commercial Launch Vehicle with Application of GPS Technologies
Mechanical and Automobile
Department, School of Engineering and Technology, Sharda University,
Greater Noida, Uttar Pradesh, 201301, India.
ABSTRACT
In this article have been proposed the design objectives for an integrated guidance system of a commercial launch vehicle with application of GPS technologies and has been set a technical problem of the conceptual design of an integrated navigation system for the space launch vehicle qualified to inject small artificial Earth satellites into low and medium circular orbits. The conceptual design of the integrated navigation system based on GPS technology involves determination of its structure, models and algorithms, providing the required accuracy and reliability in injecting payloads with due regard to restrictions on weight and dimensions of the system.